High-strength non-porous easy-to-pull airplane box

Abstract

The utility model discloses a high-strength holeless easy-to-pull airplane box which comprises a bottom plate, two sides of the bottom plate are respectively connected with a first side plate and a second side plate, two sides of the middle of the bottom plate are connected with a third side plate, one end of the first side plate is connected with a first folded plate, one end of the second side plate is connected with a cover plate, and two sides of the cover plate are connected with wing plates. According to the airplane box, the box body can be assembled without additionally arranging a clamping block and a clamping groove, the overall attractiveness is improved, the assembling steps of the airplane box are simplified, and practicability is high. Through cooperative use of the pulling plate and the connecting plate, when a product is assembled, only the third side plate needs to be bent, synchronous bending of the first side plate, the second side plate and the third side plate can be achieved, the assembling steps of the airplane box are further simplified, and then the assembling efficiency is greatly improved.

Description

Technical Field

[0001] This utility model relates to the field of aircraft box technology, specifically a high-strength, hole-free, easy-open aircraft box. Background Technology

[0002] With the rapid development of the internet and its relatively low barriers to entry, the number of individual business owners and small merchants opening online stores has surged. Preventing damage to goods during the shipping process is a crucial consideration, leading more and more merchants to choose relatively inexpensive and cost-effective corrugated boxes as their preferred packing containers. Furthermore, the ability to print store names and addresses enhances brand awareness and increases customer loyalty. However, current corrugated box designs have certain flaws, including the need for slots at the bottom for assembly and the requirement for individual bending of each component, resulting in a lack of interconnectivity.

[0003] As disclosed in the prior art, utility model CN215884421U discloses a handle-type airplane box, belonging to the field of packaging box processing. It mainly includes an airplane box body, which comprises a front baffle and a bottom plate. The front baffle of the airplane box body has a handle assembly integrally formed with the airplane box body and an insertion hole that mates with the handle assembly. The handle assembly includes two symmetrically arranged handle plates, which are respectively connected to handle baffle one and handle baffle two. Handle baffle one is connected to the front baffle of the airplane box body, and the handle plate has a handle hole. This utility model adds a handle assembly integrally formed with the airplane box body. After simple folding, the airplane box has a built-in handle, greatly reducing manufacturing steps, lowering production costs, and improving product packaging efficiency. This utility model is mainly used for product packaging.

[0004] The present invention relates to a folding aircraft box, with publication number CN211810666U, and to existing technologies.

[0005] The grooved bottom of the box affects the overall aesthetics, and the assembly of the box is time-consuming and labor-intensive, resulting in low efficiency during large-scale assembly. Therefore, we propose a high-strength, hole-free, easy-open airplane box to solve the above problems. Utility Model Content

[0006] The purpose of this invention is to provide a high-strength, non-porous, easy-open airplane box to solve the problems mentioned in the background art.

[0007] To achieve the above objectives, the present invention provides the following technical solution: a base plate, with a first side plate and a second side plate connected to both sides of the base plate, and a third side plate connected to both sides of the middle portion of the base plate. A first folding plate is connected to one end of the first side plate, and a cover plate is connected to one end of the second side plate. Wing plates are connected to both sides of the cover plate.

[0008] Preferably, one end of the first folding plate is connected to a first clamping plate, one end of the third side plate is connected to a second folding plate, and one end of the second folding plate is connected to a second clamping plate.

[0009] Preferably, one end of the cover plate is connected to an insert plate, and one side of the second card plate is connected to a pressure plate.

[0010] Preferably, the sidewalls of the first side plate and the second side plate are connected by a connecting plate, and the sidewall of the third side plate is connected by a pull plate.

[0011] Preferably, the connecting plate is fixedly connected to the side wall of the pull plate.

[0012] Preferably, a pull block is provided at one end of the cover plate adjacent to the insert plate, and a groove is provided at one end of the insert plate adjacent to the cover plate, with the pull block matching the size of the groove.

[0013] Compared with the prior art, the beneficial effects of this utility model are:

[0014] 1. This high-strength, hole-free, easy-open airplane box can be assembled without the need for additional snap-fit ​​blocks and slots, improving the overall aesthetics and simplifying the assembly process, making it highly practical.

[0015] 2. This high-strength, hole-free, easy-open aircraft box, through the combined use of the pull plate and connecting plate, allows the first, second, and third side plates to be bent simultaneously by simply bending the third side plate during assembly. This further simplifies the assembly process and greatly improves assembly efficiency. Attached Figure Description

[0016] Figure 1 This is a schematic diagram of the structure of this utility model;

[0017] Figure 2 This is a schematic diagram showing the unfolded structure of this utility model;

[0018] Figure 3 This is a schematic diagram of the structure of this utility model in use.

[0019] In the diagram: 1. Base plate; 2. First side plate; 3. Second side plate; 4. First folding plate; 5. Cover plate; 6. Wing plate; 7. Insert plate; 8. Groove; 9. Pull block; 10. First clamping plate; 11. Connecting plate; 12. Pulling plate; 13. Third side plate; 14. Second folding plate; 15. Second clamping plate; 16. Pressure plate. Detailed Implementation

[0020] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0021] This utility model provides a technical solution for a high-strength, hole-free, easy-open airplane box:

[0022] Example:

[0023] like Figure 1 , Figure 2 and Figure 3 As shown, it includes a base plate 1, with a first side plate 2 and a second side plate 3 connected to both sides of the base plate 1, and a third side plate 13 connected to both sides of the middle part of the base plate 1. A first folding plate 4 is connected to one end of the first side plate 2, and a cover plate 5 is connected to one end of the second side plate 3. Wing plates 6 are connected to both sides of the cover plate 5.

[0024] One end of the first folding plate 4 is connected to the first clamping plate 10, one end of the third side plate 13 is connected to the second folding plate 14, and one end of the second folding plate 14 is connected to the second clamping plate 15.

[0025] One end of the cover plate 5 is connected to the insert plate 7, and one side of the second card plate 15 is connected to the pressure plate 16.

[0026] The first side plate 2 and the second side plate 3 are connected by a connecting plate 11, and the third side plate 13 is connected by a pull plate 12.

[0027] The connecting plate 11 is fixedly connected to the side wall of the pull plate 12.

[0028] In this embodiment, during assembly, the first side plate 2, the second side plate 3, and the third side plate 13 are first bent to be perpendicular to the base plate 1. Then, the second folding plate 14 is bent horizontally towards the base plate 1, and the second clamping plate 15 is bent so that it fits against the base plate 1. Then, the first folding plate 4 is bent horizontally towards the base plate 1, at which point the pressure plate 16 is clamped and limited between the first folding plate 4 and the first side plate 2. Then, the first clamping plate 10 is bent so that it fits against the base plate 1. At this point, the first clamping plate 10 and the second side plate 2... The ends of the card plates 15 abut against each other to achieve a limiting effect and stabilize the shape of the box. Then, the wing plates 6 and the insert plates 7 are bent vertically towards the cover plate 5, and then the cover plate 5 is bent vertically towards the bottom plate 1, thereby closing the top opening of the aircraft box through the cover plate 5. At this time, the wing plates 6 are inserted into one side of the second folding plate 14, and the insert plates 7 are inserted into one side of the first folding plate 4, thereby limiting the cover plate 5. This product can assemble the box without the need for additional snap-fit ​​blocks and snap-fit ​​slots, which improves the overall aesthetics and simplifies the assembly steps of the aircraft box, making it highly practical.

[0029] During production, the connecting plate 11 is glued to the first side plate 2 and the second side plate 3 by machine gluing and pressing. After the product is put into use, the third side plate 13 is bent to be perpendicular to the bottom plate 1 by manpower. At this time, the third side plate 13 will pull the connecting plate 11 through the pull plate 12, and then pull the first side plate 2 and the second side plate 3. When the third side plate 13 is bent to be perpendicular to the bottom plate 1, the first side plate 2 and the second side plate 3 will be pulled up. Therefore, during product assembly, only the third side plate 13 needs to be bent to achieve the synchronous bending of the first side plate 2, the second side plate 3 and the third side plate 13, which further simplifies the assembly steps of the aircraft box and greatly improves the assembly efficiency.

[0030] Among them, such as Figure 3 As shown, a pull block 9 is provided at one end of the cover plate 5 adjacent to the insert plate 7, and a groove 8 is provided at one end of the insert plate 7 adjacent to the cover plate 5. The pull block 9 and the groove 8 are the same size.

[0031] In this embodiment, the pull block 9 facilitates the pulling of the cover plate 5, thereby making it easier to open and use the aircraft box, further improving the ease of use of the product.

[0032] In the description of this utility model, it should also be noted that, unless otherwise explicitly specified and limited, the terms "set," "install," "connect," and "link" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; and they can refer to the internal connection of two components. Those skilled in the art can understand the specific meaning of the above terms in this utility model according to the specific circumstances.

[0033] Although embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. A high-strength, non-porous, easy-open airplane box, comprising a base plate (1), characterized in that: The bottom plate (1) is connected to a first side plate (2) and a second side plate (3) on both sides respectively. The bottom plate (1) is connected to a third side plate (13) on both sides of the middle part. The first side plate (2) is connected to a first folding plate (4) at one end. The second side plate (3) is connected to a cover plate (5) at one end. The cover plate (5) is connected to wing plates (6) on both sides.

2. The high-strength, non-porous, easy-open airplane box according to claim 1, characterized in that: One end of the first folding plate (4) is connected to a first clamping plate (10), one end of the third side plate (13) is connected to a second folding plate (14), and one end of the second folding plate (14) is connected to a second clamping plate (15).

3. A high-strength, non-porous, easy-open airplane box according to claim 2, characterized in that: One end of the cover plate (5) is connected to the insert plate (7), and one side of the second clamping plate (15) is connected to the pressure plate (16).

4. A high-strength, non-porous, easy-open airplane box according to claim 1, characterized in that: The first side plate (2) and the side wall of the second side plate (3) are connected by a connecting plate (11), and the side wall of the third side plate (13) is connected by a pull plate (12).

5. A high-strength, non-porous, easy-open airplane box according to claim 4, characterized in that: The connecting plate (11) is fixedly connected to the side wall of the pull plate (12).

6. A high-strength, non-porous, easy-open airplane box according to claim 3, characterized in that: A pull block (9) is provided at one end of the cover plate (5) adjacent to the insert plate (7), and a groove (8) is provided at one end of the insert plate (7) adjacent to the cover plate (5). The pull block (9) is the same size as the groove (8).

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